FIELD: engines and pumps.
SUBSTANCE: claimed housing comprises the stiff thin-wall shell secured to the holder and having the jet nozzle inlet and outlet and curvilinear sire located there between at the shell outer side. Curvilinear site has the straight section located at 4-12 degrees to the shell central axis.
EFFECT: higher lift.
5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HOUSING OF JET ENGINE MOUNTED UNDER AIRCRAFT WING | 2014 |
|
RU2563097C1 |
| HOUSING OF JET ENGINE MOUNTED ABOVE AIRCRAFT WING | 2014 |
|
RU2564260C1 |
| JET ENGINE HOUSING | 2014 |
|
RU2556411C1 |
| WIDE-BODY AIRCRAFT WING (VERSIONS) | 2014 |
|
RU2568627C1 |
| AIRCRAFT WING | 2014 |
|
RU2554026C1 |
| AIRCRAFT | 2012 |
|
RU2503590C1 |
| AIRCRAFT WING | 2013 |
|
RU2539440C1 |
| AIRCRAFT WING | 2014 |
|
RU2576845C1 |
| AMPHIBIOUS CRAFT | 2014 |
|
RU2563096C1 |
| AIRCRAFT WING | 2009 |
|
RU2404904C1 |
